An electronic display for an aerial device is provided. The electronic display replaces a traditional load chart including the operational parameters of the aerial device being used. The electronic display electrically connected with a computer control system connected to a sensor for collecting at least one piece of data relating to the operational parameters of the aerial device. The computer control system calculating the current operational parameter of the aerial device based on the at least one piece of data collected by the sensor and updating the operational parameters of the aerial device and displaying a graphical representation of the updated operational parameters on the electronic display.

A vehicle includes a chassis defining a longitudinal axis, a cab coupled to the chassis, a front axle coupled to the chassis, a rear axle coupled to the chassis, a body assembly coupled to the chassis, and an implement. The body assembly defines a recess that includes a plurality of angled portions. The plurality of angled portions extend laterally outward at a downward angle away from the longitudinal axis. The implement has a proximal end disposed within the recess. The plurality of angled portions at least partially facilitate the implement in traveling through at least one of a sweep angle range or a depression angle range.